INS-U-OEM
GPS-Aided OEM INS with Air Data Computer
The Inertial Labs GPS-Aided Inertial Navigation System (INS-U-OEM) is OEM version of new generation, fully-integrated, combined GPS, GLONASS, GALILEO, QZSS and BEIDOU GNSS and high-performance strapdown system, that determines position, velocity and absolute orientation (Heading, Pitch and Roll) for any device on which it is mounted. Horizontal and Vertical Position, Velocity and Orientation are determined with high accuracy for both motionless and dynamic applications.
Description
- INS, AHRS and ADC (Air Data Computer) output data
- Multi frequency and Multi constellations GNSS Receiver
- GPS, GLONASS, GALILEO, QZSS and BEIDOU GNSS
- Designed for fixed-wing and multi-rotor Aerial Platforms
- Two Barometers for Indicated Airspeed
- Position accuracy = 1 cm (RTK)
- Heading accuracy = 0.3 deg (RTK, Dynamic)
- Pitch & Roll accuracy = 0.1 deg (RTK, Dynamic)
- Gyro-compensated, embedded Fluxgate magnetic compass
- Optional external Stand-Alone Magnetic Compass
- Small Size, light weight, low power • Affordable price
The Inertial Labs INS-U-OEM utilizes advanced single antenna GNSS receiver, two barometers, magnetometers, 3-axes each of calibrated in full operational temperature range Advanced MEMS Accelerometers and Gyroscopes to provide accurate Position, Velocity, Heading, Pitch and Roll of the device under measure.
INS-U-OEM contains Inertial Labs new on-board sensors fusion filter, state-of-the-art navigation and guidance algorithms and calibration software.
KEY FEATURES, BENEFITS & FUNCTIONALITY
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Commercially exportable GPS-Aided Inertial Navigation System
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3-in-1 strapdown system: INS + AHRS + ADC (Air Data Computer)
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Embedded in-flight calibration
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UBlox ZED-F9P F9 High Precision GNSS Module
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Small size & light weight & low power
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GPS, GLONASS, GALILEO, BEIDOU, QZSS, RTK supported signals
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Total and static pressure sensors for calculating Indicated Airspeed
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Embedded or External Inertial Labs Magneto-Inductive and Mini-Fluxgate
magnetometers (compass)
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GNSS measurements and IMU raw data for post-processing
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Advanced, extendable, embedded Kalman Filter-based sensor fusion algorithms
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State-of-the-art algorithms for different dynamic motions of Helicopters, and UAV
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Specifications
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Other specifications
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Export restrictions
ITAR Free
Graphical user interface
Y
Typical application
Fixed-wing, VTOL UAV
Distinguishable features
Low cost, Air Data Computer (ADC)
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Environmental
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Non-operating shock tolerance [g]
3000
Operating shock tolerance [g]
1500
Min. operating temperature [°C]
-40
Max. operating temperature [°C]
85
Max. rotation speed [deg/s]
950
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Software
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Name
GUI Software
Filtering
Y
Adaptable filter strength
Kalman
Adaptable input signals
Y
Integrity monitoring of position input
Y
Integrity monitoring of log input
Y
Max. number of position input signals
10
Max. number of log input signals
10
Maximum latency of log input [ms]
3
Maximum latency of position input [ms]
3
Uncertainty indicators given in output
Yes
Uncertainty of time stamp for output [ms]
0.02
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GNSS aided uncertainty
-
Heading [deg]
0.3
Pitch [deg]
0.05
Roll [deg]
0.05
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General
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Type of application
Air
Year of initial development
2020
Height [mm]
19.9
Width [mm]
37.2
Length [mm]
65
Weight [kg]
0.1
Min. Voltage (DC)
5
Max. Voltage (DC)
32
Power consumption [W]
1
Mean time between failures [hr]
100000
Type of accelerometer
MEMS
Type of gyro
MEMS
Removable from base plate
N
Moving parts
N
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GNSS Positioning Sensor
-
Number of integrated GNSS receivers and antenna ports
1
No. channels p receiver
184
Tracked satellite signals
All Constellations
SBAS differential signals
Yes
RTK Network Compatibility
Yes
Update rate [ Hz ]
200
Cold start [ seconds ]
50
Hot start [ seconds ]
30
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Data formats
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NMEA formats
NMEA 0183
RTCM
Y
Other
Binary, ASCII
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Inertial Measurement Unit
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Accelerometer bias [µ-g]
2
gyro bias [deg/hr]
2
Calibration procedure
In-fligth
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GNSS positional accuracy
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Horizontal Position Accuracy [ RMS in cm ]
150
Horizontal Position Accuracy (RTK) [ RMS in cm ]
1